EP3383741A4 - Electronic rudder bias system - Google Patents

Electronic rudder bias system Download PDF

Info

Publication number
EP3383741A4
EP3383741A4 EP16871462.4A EP16871462A EP3383741A4 EP 3383741 A4 EP3383741 A4 EP 3383741A4 EP 16871462 A EP16871462 A EP 16871462A EP 3383741 A4 EP3383741 A4 EP 3383741A4
Authority
EP
European Patent Office
Prior art keywords
bias system
rudder bias
electronic rudder
electronic
rudder
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP16871462.4A
Other languages
German (de)
French (fr)
Other versions
EP3383741A1 (en
EP3383741B1 (en
Inventor
Jukka Matti Hirvonen
Nilesh Arun SAHANI
Jeremy Nathaniel MONTGOMERY
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Honda Patents and Technologies North America LLC
Original Assignee
Honda Patents and Technologies North America LLC
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Honda Patents and Technologies North America LLC filed Critical Honda Patents and Technologies North America LLC
Publication of EP3383741A1 publication Critical patent/EP3383741A1/en
Publication of EP3383741A4 publication Critical patent/EP3383741A4/en
Application granted granted Critical
Publication of EP3383741B1 publication Critical patent/EP3383741B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D31/00—Power plant control; Arrangement thereof
    • B64D31/02—Initiating means
    • B64D31/06—Initiating means actuated automatically
    • B64D31/10—Initiating means actuated automatically for preventing asymmetric thrust upon failure of one power plant
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/02—Initiating means
    • B64C13/16—Initiating means actuated automatically, e.g. responsive to gust detectors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24—Transmitting means
    • B64C13/38—Transmitting means with power amplification
    • B64C13/50—Transmitting means with power amplification using electrical energy
    • B64C13/503—Fly-by-Wire
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Feedback Control In General (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)
  • Retarders (AREA)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
EP16871462.4A 2015-12-03 2016-12-01 Electronic rudder bias system Active EP3383741B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US201562262466P 2015-12-03 2015-12-03
PCT/US2016/064312 WO2017095980A1 (en) 2015-12-03 2016-12-01 Electronic rudder bias system

Publications (3)

Publication Number Publication Date
EP3383741A1 EP3383741A1 (en) 2018-10-10
EP3383741A4 true EP3383741A4 (en) 2018-12-05
EP3383741B1 EP3383741B1 (en) 2020-06-10

Family

ID=58797749

Family Applications (1)

Application Number Title Priority Date Filing Date
EP16871462.4A Active EP3383741B1 (en) 2015-12-03 2016-12-01 Electronic rudder bias system

Country Status (5)

Country Link
US (1) US10745141B2 (en)
EP (1) EP3383741B1 (en)
BR (1) BR112018011197B1 (en)
CA (1) CA3006770C (en)
WO (1) WO2017095980A1 (en)

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2219775A (en) * 1988-03-22 1989-12-20 British Aerospace Control systems for aircraft
US5657949A (en) * 1995-05-10 1997-08-19 The Boeing Company Method and apparatus for providing a dynamic thrust asymmetry rudder compensation command with no direct thrust measurement
US6586901B1 (en) * 2000-06-21 2003-07-01 Honeywell International Inc. Methods and apparatus suitable for facilitating control of an aircraft rudder

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4935682A (en) * 1988-08-11 1990-06-19 The Boeing Company Full authority engine-out control augmentation subsystem
FR2854962B1 (en) * 2003-05-14 2005-08-05 Airbus France METHOD AND DEVICE FOR CONTROLLING AN AIRCRAFT
US7984880B2 (en) * 2007-10-09 2011-07-26 Embraer-Empresa Brasileira De Aeronautica S.A. Mechanisms and methods for providing rudder control assist during symmetrical and asymmetrical thrust conditions
US8352099B1 (en) * 2009-07-09 2013-01-08 The Boeing Company Varying engine thrust for directional control of an aircraft experiencing engine thrust asymmetry
DE102013101602A1 (en) * 2013-02-18 2014-09-04 Airbus Operations Gmbh Airplane, has thrust creation units arranged to provide independent pushing force with thrust direction vector provided with spacing to yaw axis of airplane main portion, to reduce thrust asymmetry of airplane main portion
US9889944B2 (en) * 2013-08-28 2018-02-13 United Technologies Corporation Multi-engine aircraft thrust balancing

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2219775A (en) * 1988-03-22 1989-12-20 British Aerospace Control systems for aircraft
US5657949A (en) * 1995-05-10 1997-08-19 The Boeing Company Method and apparatus for providing a dynamic thrust asymmetry rudder compensation command with no direct thrust measurement
US6586901B1 (en) * 2000-06-21 2003-07-01 Honeywell International Inc. Methods and apparatus suitable for facilitating control of an aircraft rudder

Also Published As

Publication number Publication date
BR112018011197B1 (en) 2023-03-14
WO2017095980A1 (en) 2017-06-08
CA3006770C (en) 2023-08-22
BR112018011197A2 (en) 2018-11-21
CA3006770A1 (en) 2017-06-08
EP3383741A1 (en) 2018-10-10
EP3383741B1 (en) 2020-06-10
US20190009922A1 (en) 2019-01-10
US10745141B2 (en) 2020-08-18

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